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Fluid dynamics / Washout / Stall / Wing twist / Chord / Lift-induced drag / Stall strips / Aerospace engineering / Aerodynamics / Aviation


Wing Taper Considerations Tapering a wing planform gives a number of significant aerodynamic and structural advantages, but it can also cause problems if overdone. Consider three AR = 10 wings of the same span and area, but different taper ratios λ = ctip /croot . When operated at some overall lift
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Document Date: 2013-09-29 08:11:09


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